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Journal Articles

Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

A. R. Wadia, J. D. Niedermeier, P. N. Szucs, N. G. Cormier, D. W. Crall, D. C. Rabe

Publisher: ASME

J. Turbomach. August 2019, 141(8): 081012.

Paper No: TURBO-18-1183

https://doi.org/10.1115/1.4043574

Published Online: May 23, 2019

View Article titled, Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

Topics: Blades, Design, Rotors, Stators

Proceedings Papers

Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

A. R. Wadia, J. D. Niedermeier, P. N. Szucs, N. G. Cormier, D. W. Crall, D. C. Rabe

Proc. ASME. GT2018, Volume 2A: Turbomachinery, V02AT39A013, June 11–15, 2018

Publisher: American Society of Mechanical Engineers

Paper No: GT2018-75562

https://doi.org/10.1115/GT2018-75562

View Paper titled, Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

Topics: Design, Rotors, Testing, Blades, Deflection, Airfoils, Compressors, Fans, Flow (Dynamics), Rotation

Proceedings Papers

Acquisition of F-100(3) High Pressure Compressor Entrance Profiles

D. C. Rabe, W. W. Copenhaver, M. S. Perry

Proc. ASME. GT1982, Volume 1: Turbomachinery, V001T01A071, April 18–22, 1982

Publisher: American Society of Mechanical Engineers

Paper No: 82-GT-215

https://doi.org/10.1115/82-GT-215

View Paper titled, Acquisition of F-100(3) High Pressure Compressor Entrance Profiles

Topics: Compressors, High pressure (Physics), Pressure, Uncertainty, Air flow, Air Force, Data acquisition systems, Engines, Flow (Dynamics), Gas turbines

Proceedings Papers

Forward Swept Rotor Studies in Multistage Fans With Inlet Distortion

A. R. Wadia, P. N. Szucs, D. W. Crall, D. C. Rabe

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 11-21, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30326

https://doi.org/10.1115/GT2002-30326

View Paper titled, Forward Swept Rotor Studies in Multistage Fans With Inlet Distortion

Topics: Fans, Rotors, Inlet guide vanes, Stability, Blades, Flow (Dynamics), High pressure (Physics), Military systems, Testing

Proceedings Papers

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

A. J. Sanders, K. K. Hassan, D. C. Rabe

Proc. ASME. GT2003, Volume 4: Turbo Expo 2003, 339-348, June 16–19, 2003

Publisher: American Society of Mechanical Engineers

Paper No: GT2003-38353

https://doi.org/10.1115/GT2003-38353

View Paper titled, Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

Topics: Flutter (Aerodynamics), Computational fluid dynamics, Clearances (Engineering), Computer simulation, Cycles, Design, Pressure transducers, Strain gages, Vibration

Proceedings Papers

Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor

D. C. Rabe, C. Hah

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 1141-1153, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30641

https://doi.org/10.1115/GT2002-30641

View Paper titled, Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor

Topics: Compressors, Flow (Dynamics), Boundary layers, Pressure, Steady state

Journal Articles

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

A. J. Sanders, K. K. Hassan, D. C. Rabe

Publisher: ASME

J. Turbomach. January 2004, 126(1): 166–174.

https://doi.org/10.1115/1.1645532

Published Online: March 26, 2004

View Article titled, Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

Topics: Computational fluid dynamics, Flutter (Aerodynamics), Pressure, Clearances (Engineering), Simulation, Flow (Dynamics), Cycles

Journal Articles

Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor

D. W. Thompson, P. I. King, D. C. Rabe

Publisher: ASME

J. Turbomach. July 1998, 120(3): 477–486.

https://doi.org/10.1115/1.2841743

Published Online: July 1, 1998

View Article titled, Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor

Topics: Axial flow, Compressors, Rotors, Clearances (Engineering), Flow (Dynamics), Design, Engineers, Inlet guide vanes, Pressure

Journal Articles

Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor

C. Hah, D. C. Rabe, T. J. Sullivan, A. R. Wadia

Publisher: ASME

J. Turbomach. April 1998, 120(2): 233–246.

https://doi.org/10.1115/1.2841398

Published Online: April 1, 1998

View Article titled, Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor

Topics: Compressors, Flow (Dynamics), Rotors, Blades, Pressure, Shock (Mechanics), Boundary layers, Viscous flow, Boundary-value problems, Chords (Trusses)

Journal Articles

Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan

S. R. Manwaring, D. C. Rabe, C. B. Lorence, A. R. Wadia

Publisher: ASME

J. Turbomach. October 1997, 119(4): 665–676.

https://doi.org/10.1115/1.2841176

Published Online: October 1, 1997

View Article titled, Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan

Topics: Acoustics, Aerodynamics, Airfoils, Blades, Boundary layers, Dynamics (Mechanics), Flow (Dynamics), Pressure, Pressure transducers, Resonance

Journal Articles

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

D. C. Rabe, A. J. Wennerstrom, W. F. O’Brien

Publisher: ASME

J. Turbomach. July 1988, 110(3): 386–392.

https://doi.org/10.1115/1.3262208

Published Online: July 1, 1988

View Article titled, Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

Topics: Boundary layers, Compressors, Rotors, Shock waves, Blades, Lasers, Air Force, Chords (Trusses), Flow (Dynamics), Shear (Mechanics)

Journal Articles

Verification of Compressor Data Accuracy by Uncertainty Analysis and Testing Methods

N. D. Poti, D. C. Rabe

Publisher: ASME

J. Turbomach. April 1988, 110(2): 265–269.

https://doi.org/10.1115/1.3262190

Published Online: April 1, 1988

View Article titled, Verification of Compressor Data Accuracy by Uncertainty Analysis and Testing Methods

Topics: Compressors, Testing, Uncertainty analysis, Uncertainty, Air Force

Journal citation

NARROW

Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

Aerodynamic Design and Testing of an Imbedded Forward Swept Rotor in a Two-Stage Transonic Fan

Acquisition of F-100(3) High Pressure Compressor Entrance Profiles

Forward Swept Rotor Studies in Multistage Fans With Inlet Distortion

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor

Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor

Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

Verification of Compressor Data Accuracy by Uncertainty Analysis and Testing Methods

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